View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 66690U 26145.15520046 +.00000000 +00000-0 +21213-3 0 00003
2 66690 97.4187 218.9077 0006399 84.9138 275.2827 15.18812246 00
| Epoch (UTC): | 25 May 2026 03:43:29 |
| Eccentricity: | 0.0006399 |
| inclination: | 97.4187° |
| perigee height: | 505 km |
| apogee height: | 514 km |
| right ascension of ascending node: | 218.9077° |
| argument of perigee: | 84.9138° |
| revolutions per day: | 15.18812246 |
| mean anomaly at epoch: | 275.2827° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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